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PETREL, 69503

Orbit data source: Space-Track

PETREL, 69503 is a Japanese payload satellite in SSO that was launched on Fri, 12 Jun 2026 UTC via a H3-30S launch vehicle from the Tanegashima Space Center (TNSTA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
69503, 2026-132B
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
SCITOK
Mission
Operational spacecraft
Bus & Motor
PETREL, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
2026-06-12 (1 month ago)
Launch vehicle
H3-30S
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 PETREL
1 69503U 26132B   26193.05103872  .00001007  00000-0  87421-4 0  9998
2 69503  97.6914 256.4116 0014144 177.7570 182.3719 14.99182309  4500
Epoch: 2026-07-12T01:13Z
TLE epoch observation values (Epoch: 2026-07-12T01:13:29.745Z)
Latitude
-0.00002°
Longitude
-51.9178°
Altitude
582.296 km
Speed
7.564 km/s
True Right ascension
17h 05m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:45:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.25 km
Perigee altitude
556.605 km
Semi-major axis
6,944.564 km
Eccentricity
0.00141
Inclination
97.6914°
RAAN
256.4116°
Arg. of periapsis
177.757°
True anomaly
182.3652°
Mean anomaly
182.3719°
Eccentric anomaly
182.36855°
Mean motion
3.75038 °/min
Orbital period
95.99 mins
BSTAR
0.000087421
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Other satellites on launch #132 in the year 2026 (2026-06-12 UTC)

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